NASA / MEMO 5-16-59A
Lopez,Armando E,Buell,Donald A
THE STATIC AND DYNAMIC ROTARY STABILITY DERIVATIVES AT SUBSONIC SPEEDS ON AN AIRPLANE MODEL HAVING WING AND TAIL SURFACES SWEPT BACK 45
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.- Nasa, Washington, D.C., 1959
.- 75 .
Bound With Nasa Memo 5-12-59a,5-18-59a-5-20-59a Lack No. 13-15,17,19
Author Added Entry:
Tinling,Bruce E;
Copy Details:
Acc. No.: TR11440, Full Call No.: NASA MEMO 5-16-59A, Item type: Technical Report , Location: General Stacks,
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